Not Applicable
Not Applicable
Not Applicable
1. Field of the Invention
Same as typical for existing four and two cycle engines.
U.S. CL . . . 123/44C; 123/44D; 123/45R; 123/54.3
2. Background Art
Existing four cycle engines utilize crankshafts that provide little mechanical advantage, have restricted intake and exhaust cycles, existing four cycle engines must store energy in flywheels to smooth power strokes, existing four cycle engines can provide only one power stroke per cylinder every other revolution and have strokes that are limited to each being ninety degrees of revolution. Two cycle engines are polluters.
Attempts at designing rotary engines with some, most or all of the following elements; reciprocating pistons, rotating cylinders, cams and ported engine housings, have failed to produce marketable designs because they would not produce the amount power required, have much concentric motion, were limited to strokes of ninety degrees in duration, were suitable only for aircraft, were too complex or could not be properly cooled or lubricated, or could not be practically manufactured.
In this engine the resultant of the power stroke and resistance to the same by channels cast in the engine housings forces rotation of an upper restraining ring, pistons with rings, cylinders, channel rollers, slotted restraining plates with power shafts, connecting rods with side shafts, restraining hub and threaded spacer bars. Cylinders rotate past exhaust and intake ports in the cylinder head while channel rollers in the channels force the cycles. Engine provides a minimum of one power stroke for every cylinder every revolution with unrestricted exhaust and intake strokes. A large percentage of the mass of the engine is rotating. The advantage of this engine is no flywheel is required, complete unrestricted exhaust and intake cycles, a minimum of one power stroke every cylinder every revolution, variability in the duration of stokes, fuel efficiency, and simplified manufacturing and it produces more power relative to its weight and displacement.
Ref. No. Description
Fuel systems are not addressed in this application due to the wide variance of fuels available and the need to adapt these systems to the fuels properties.
Cooling systems are not addressed in this application due to the wide variance of fuels available and need to adapt these systems to the fuels properties.
Lubrication systems are not addressed in this application due to the wide variance of fuel available and the need to adapt these systems to the fuels properties.
Ignition and electrical systems are not addressed in this application due to the wide variance of fuel available and the need to adapt these systems to the fuels properties.
Elements of the above systems, subdivision of multifunctional elements and minor changes to the elements are not limited by this description or the claims.
A rotary four-cycle internal combustion engine that is an assemblage of single and multifunctional fixed elements comprising
a cylinder head 1 (
a duality of engine housings with channels 2 (
and an assemblage of single and multifunctional rotating elements comprising
a duality of power shaft bearings 3 (
a seal and compression rings 4 (
an upper restraining ring 5 (
a plurality of cylinders 6 (
a plurality of pistons with rings 7 (
a plurality of threaded spacer bars 8 (
a plurality of connecting rods with side shafts 11 (
a duality of slotted restraining plates with power shafts 12 (
a plurality of restraining plate slot bearings 14 (
a plurality of channel bearings 17 (
a plurality of threaded holes with fasteners 18 (
An engine having engine housings with channels 2 fastened to cylinder head 1, with thickened 2a and 2c and channel portions 2b turned inwardly, inclosing all rotating elements excepting an outwardly portion of power shaft portions 12b,
having channel portions 2b with a center line alignment two stoke lengths plus half the diameter of side shaft portions 11a from axis of rotation at beginning of combustion and intake cycles and a stoke length plus half the diameter of side shaft portions 11a from axis of rotation at beginning of compression and exhaust cycles and with degrees of each rotation between the cycles, as drawn, being ninety,
having channel portions 2b concentrically resisting inwardly forces applied to channel rollers 16 during combustion cycles forcing channel rollers 16 to roll within channel portions 2b alignment transitioning inwardly a stroke length,
An engine having a cylinder head 1 providing a surface to seal top of a cylinder 6 during compression and combustion cycles, providing access to cylinders 6 by ignition and/or fuel injection devises and a singularity or plurality each, beginning at beginning and ending at end of exhaust and intake cycles, of exhaust and intake ports serially located in correspondence with cycles prescribed by alignment of channel portions 2b.
An engine having an assemblage of rotating elements consisting of an upper restraining ring 5, a seal and compression rings 4, a plurality of cylinders 6, a plurality of threaded spacer bars 8, a restraining hub 9, a plurality of receiving cylinders 10, a plurality of restraining slots 13, and a duality of slotted restraining plates with power shafts 12 fastened together in rigid parallel plane radial coaxial alignment and
a plurality of pistons 7, a plurality of connecting rods with side shafts 11, a plurality of channel roller bearings 15 and a plurality of channel rollers 16 in parallel plane radially reciprocating coaxial alignment and
having cylinders 6 participating in a cycle and disposed for sequential entry into each cycle, pistons with rings 7 reciprocally disposed in cylinders 6, connecting rods with side shafts 11 attached to pistons with rings 7, with side shafts portions 11a passed through and restrained in restraining slots 13, attached to channel rollers 16 disposed in channel portions 2b and lower portions lib disposed in receiving cylinders.
An engine having an upper restraining ring 5 with outward ends of cylinders 6 fastened into threaded openings restraining cylinders in spaced apart coplanar radial coaxial alignment extended inwardly and having a seal with compression rings 4 between inward surface of cylinder head 1 and upper restraining rings 5 outward surface closing ports when cylinders are not present and providing tighter seal of cylinders during compression and combustion cycles.
An engine having a plurality of cylinders 6 threaded at opposing ends with cylinders 6 slightly greater in outside diameter for length of threads on outward ends, fastened into threaded openings in upper restraining ring 5 and fastened into joined pairs of threaded spacer bars 8 at inward ends providing a rigid coplanar coaxial connection between upper restraining ring 5 and threaded spacer bars 8.
An engine having a plurality of pistons with rings 7 reciprocally disposed in each cylinder 6 and aligned for a singularity or plurality of pistons 7 to be in each of the four cycle regions simultaneously and disposed for sequential entry into each cycle region,
An engine having a plurality of threaded spacer bars 8 evenly radically coplanar disposed and fastened between opposing plate portions 12a, spacing plate portions 12a apart equal to outside diameter of inward end of cylinders 6 fastened to and restraining a plurality of cylinders 6 in coplanar evenly spaced radially coplanar coaxial; alignment,
An engine having a restraining hub 9 fastened between and spacing apart, equal to the outside diameter of inward end of cylinders 6, opposing plate portions 12a and restraining receiving cylinders 10 and inwardly ends 11b in evenly spaced parallel plane radial alignment,
An engine having slotted restraining plates with power shafts 12 restraining side shaft portions 11a passed through restraining slots 13 in evenly spaced parallel plane radial reciprocating alignment, restraining joined pairs of threaded spacer bars 8, restraining slots 13 of opposing plate portions 12a and restraining hub 9 in evenly spaced parallel plane radial coaxial alignment,
having transversely offset from centers of plate portions 12a opposing power shaft portions 12b, extending through opposing power shaft bearings 3 and openings in opposing thickened circular center portions 2c, providing an axes of rotation for an assemblage of single and multifunctional rotating elements.
An engine having a plurality of connecting rods with side shafts 11 fastened to pistons with rings 7, channel roller bearings 15 and channel rollers 16 forcing fastened elements to reciprocate in unison,
transferring pressure of expanding combustion gases acting as an inward force on piston with rings 7 during combustion cycle to channel rollers 16 constrained within channel portions 2b transitioning a stoke length closer to axis of rotation, where force is concentrically resisted forcing channel rollers 16 engaged in combustion cycles to roll applying force to fastened side shafts 11a which in return is applied to sides of slots 13 inducing rotational momentum to slotted restraining plates with power shafts and fastened elements which in return is applied to side shaft portions extended though slots engaged in the remaining three cycles,
transferring force to channel rollers, which in return transfer the resisting forces constraining channel rollers 16 to alignment of channel portions 2b transitioning a stoke length more distant from the axis of rotation during exhaust cycle to pistons with rings 7 pushing pistons with rings 7 outwardly and pushing combustion gases out though an exhaust port,
transferring resisting forces constraining channel rollers 16 to alignment of channel portions 2b transitioning a stoke length closer to axis of rotation during intake cycle to pistons with rings 7 pulling pistons with rings 7 inwardly in-taking air or fuel/air mixture, and
transferring resisting forces constraining channel rollers 16 to alignment of channel portions 2b transitioning a stoke length more distant from axis of rotation during compression cycle to pistons with rings 7 pushing pistons with rings 7 outwardly compressing air or fuel/air mixtures.
Number | Date | Country | |
---|---|---|---|
Parent | 11580615 | Oct 2006 | US |
Child | 12378569 | US |